DE69100743D1 - Flugtriebwerkregelsystem ansprechend auf die Turbineneintrittstemperatur. - Google Patents

Flugtriebwerkregelsystem ansprechend auf die Turbineneintrittstemperatur.

Info

Publication number
DE69100743D1
DE69100743D1 DE91402245T DE69100743T DE69100743D1 DE 69100743 D1 DE69100743 D1 DE 69100743D1 DE 91402245 T DE91402245 T DE 91402245T DE 69100743 T DE69100743 T DE 69100743T DE 69100743 D1 DE69100743 D1 DE 69100743D1
Authority
DE
Germany
Prior art keywords
control system
engine control
inlet temperature
aircraft engine
turbine inlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
DE91402245T
Other languages
English (en)
Other versions
DE69100743T2 (de
Inventor
Jean-Pierre Maulat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69100743D1 publication Critical patent/DE69100743D1/de
Application granted granted Critical
Publication of DE69100743T2 publication Critical patent/DE69100743T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
DE91402245T 1990-08-16 1991-08-14 Flugtriebwerkregelsystem ansprechend auf die Turbineneintrittstemperatur. Expired - Fee Related DE69100743T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9010375A FR2665927B1 (fr) 1990-08-16 1990-08-16 Dispositif compensateur de temperature devant la turbine d'une turbomachine d'aviation.

Publications (2)

Publication Number Publication Date
DE69100743D1 true DE69100743D1 (de) 1994-01-20
DE69100743T2 DE69100743T2 (de) 1994-05-11

Family

ID=9399686

Family Applications (1)

Application Number Title Priority Date Filing Date
DE91402245T Expired - Fee Related DE69100743T2 (de) 1990-08-16 1991-08-14 Flugtriebwerkregelsystem ansprechend auf die Turbineneintrittstemperatur.

Country Status (4)

Country Link
US (1) US5157918A (de)
EP (1) EP0471623B1 (de)
DE (1) DE69100743T2 (de)
FR (1) FR2665927B1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19523845C2 (de) * 1995-06-30 2002-08-01 Mtu Aero Engines Gmbh Verfahren und Anordnung zur Regelung der Treibstoffzufuhr für Triebwerke
US6834226B2 (en) * 2002-09-13 2004-12-21 Elliott Energy Systems, Inc. Multiple control loop acceleration of turboalternator after reaching self-sustaining speed previous to reaching synchronous speed
US7549292B2 (en) * 2005-10-03 2009-06-23 General Electric Company Method of controlling bypass air split to gas turbine combustor
US8535140B2 (en) * 2007-12-21 2013-09-17 Cfph, Llc System and method for providing a baccarat game based on financial market indicators
FR2990002B1 (fr) * 2012-04-27 2016-01-22 Snecma Turbomachine comportant un systeme de surveillance comprenant un module d'engagement d'une fonction de protection de la turbomachine et procede de surveillance
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention
US11158140B2 (en) 2019-03-19 2021-10-26 General Electric Company Signal response monitoring for turbine engines

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3667218A (en) * 1970-03-27 1972-06-06 Gen Electric Gas turbine temperature adaptive control
DE2208040C3 (de) * 1972-02-21 1979-05-23 Robert Bosch Gmbh, 7000 Stuttgart Regelschaltung für die Prozeßtemperatur einer Gasturbine
US3902315A (en) * 1974-06-12 1975-09-02 United Aircraft Corp Starting fuel control system for gas turbine engines
US4314445A (en) * 1977-10-17 1982-02-09 Lewis Leon D Turbine engine thrust booster
GB1591217A (en) * 1977-10-17 1981-06-17 Garrett Corp Engine fuel control system
US4350008A (en) * 1979-12-26 1982-09-21 United Technologies Corporation Method of starting turbine engines
US4627234A (en) * 1983-06-15 1986-12-09 Sundstrand Corporation Gas turbine engine/load compressor power plants
US4910956A (en) * 1988-04-28 1990-03-27 United Technologies Corporation Gas turbine overtemperature protection

Also Published As

Publication number Publication date
EP0471623A1 (de) 1992-02-19
EP0471623B1 (de) 1993-12-08
FR2665927A1 (fr) 1992-02-21
FR2665927B1 (fr) 1992-10-30
DE69100743T2 (de) 1994-05-11
US5157918A (en) 1992-10-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8339 Ceased/non-payment of the annual fee